Hydraulic Arbor Design
A sealed oil capsule bulges a thin sleeve to grip a part — OD grip (expanding arbor) or ID grip (expansion chuck). Set the charge, read lift, grip pressure, torque and margins.
Updated: 7/4/2026
| Material | Category | E (Mpsi) | ν | α (ppm/°F) | σy (psi) | ρ (lb/in³) | k (W/m·K) | Eₜ (%E) | |
|---|---|---|---|---|---|---|---|---|---|
| Carbon & alloy steel | |||||||||
| Steel (E=200 GPa) | Carbon & alloy steel | 29.008 | 0.28 | 6.5 | 36,259.4 | 0.3 | 50 | — | |
| Steel A36 (structural) | Carbon & alloy steel | 29.008 | 0.26 | 6.5 | 36,259.4 | 0.3 | 50 | — | |
| Steel 1018 (cold-drawn) | Carbon & alloy steel | 29.733 | 0.29 | 6.5 | 53,664 | 0.3 | 52 | — | |
| Carbon steel 1045 (cold-drawn) | Carbon & alloy steel | 29.733 | 0.29 | 6.389 | 76,870 | 0.3 | 50 | — | |
| Alloy steel 4140 (Q&T) | Carbon & alloy steel | 29.733 | 0.29 | 6.833 | 94,999.7 | 0.3 | 42 | — | |
| Alloy steel 4340 (Q&T) | Carbon & alloy steel | 29.733 | 0.29 | 6.833 | 124,732.5 | 0.3 | 44 | — | |
| AISI 4130 (normalized) | Carbon & alloy steel | 29.733 | 0.29 | 6.778 | 63,091.4 | 0.3 | 42.7 | — | |
| AISI 8620 (normalized core, carburizing grade) | Carbon & alloy steel | 29.733 | 0.29 | 6.611 | 52,213.6 | 0.3 | 46.6 | — | |
| AISI 8620 carburized (58-62 HRC case) | Carbon & alloy steel | 29.733 | 0.29 | 6.611 | 166,793.4 | 0.3 | 46.6 | — | |
| AISI 9310 gear steel (carburized, annealed core) | Carbon & alloy steel | 29.733 | 0.29 | 6.833 | 65,267 | 0.3 | 42.6 | — | |
| AISI 1020 (as-rolled) | Carbon & alloy steel | 29.008 | 0.29 | 6.5 | 47,862.5 | 0.3 | 51.9 | — | |
| AISI 1095 spring steel (Q&T, 480C temper) | Carbon & alloy steel | 29.733 | 0.29 | 6.333 | 110,228.7 | 0.3 | 47 | — | |
| AISI 52100 bearing steel (hardened & tempered) | Carbon & alloy steel | 30.458 | 0.29 | 6.611 | 250,190.1 | 0.3 | 46.6 | — | |
| Maraging steel C250 (18Ni, aged) | Carbon & alloy steel | 26.832 | 0.3 | 5.611 | 246,564.2 | 0.3 | 19.7 | — | |
| Maraging steel C300 (18Ni, aged) | Carbon & alloy steel | 27.557 | 0.3 | 5.611 | 290,075.5 | 0.3 | 25.3 | — | |
| Nitralloy 135M (nitriding steel, Q&T core) | Carbon & alloy steel | 29.733 | 0.29 | 6.444 | 89,923.4 | 0.3 | 22 | — | |
| AISI 4150 (Q&T, 540C temper) | Carbon & alloy steel | 27.557 | 0.29 | 6.833 | 175,495.7 | 0.3 | 42 | — | |
| Alloy steel 4140 (45 HRC) | Carbon & alloy steel | 29.733 | 0.29 | 6.833 | 181,297.2 | 0.3 | 42 | — | |
| AerMet 100 (aged) | Carbon & alloy steel | 28.137 | 0.28 | 6.111 | 250,045.1 | 0.3 | 25 | — | |
| Tool steel | |||||||||
| Tool steel O1 (hardened) | Tool steel | 29.733 | 0.3 | 6.111 | 210,304.7 | 0.3 | 46 | — | |
| Tool steel A2 (hardened) | Tool steel | 29.443 | 0.29 | 5.889 | 220,457.4 | 0.3 | 26 | — | |
| Tool steel D2 (hardened) | Tool steel | 30.458 | 0.29 | 5.778 | 217,556.6 | 0.3 | 20 | — | |
| Tool steel H13 (hot-work, hardened ~50 HRC) | Tool steel | 30.458 | 0.3 | 5.778 | 185,068.2 | 0.3 | 24.6 | — | |
| Tool steel S7 (shock-resisting, hardened ~54 HRC) | Tool steel | 30.023 | 0.3 | 7 | 234,961.1 | 0.3 | 24.6 | — | |
| Stainless | |||||||||
| Stainless 304 | Stainless | 27.992 | 0.29 | 9.611 | 31,183.1 | 0.3 | 16 | — | |
| Stainless 316 | Stainless | 27.992 | 0.27 | 8.889 | 42,060.9 | 0.3 | 16 | — | |
| Stainless 410 (tempered) | Stainless | 29.008 | 0.29 | 5.5 | 60,190.7 | 0.3 | 25 | — | |
| Stainless 17-4 PH H900 | Stainless | 28.572 | 0.27 | 6 | 169,694.2 | 0.3 | 18 | — | |
| Stainless 303 (annealed) | Stainless | 27.992 | 0.3 | 9.611 | 34,809.1 | 0.3 | 16.2 | — | |
| Stainless 321 (annealed) | Stainless | 27.992 | 0.27 | 9.222 | 29,732.7 | 0.3 | 16.1 | — | |
| Stainless 347 (annealed) | Stainless | 27.992 | 0.28 | 9.222 | 29,732.7 | 0.3 | 16.3 | — | |
| Stainless 430 (annealed) | Stainless | 29.008 | 0.3 | 5.778 | 44,961.7 | 0.3 | 26.1 | — | |
| Stainless 440C (hardened) | Stainless | 29.008 | 0.28 | 5.667 | 275,571.7 | 0.3 | 24.2 | — | |
| Stainless 2205 duplex (annealed) | Stainless | 27.557 | 0.3 | 7.222 | 65,267 | 0.3 | 19 | — | |
| Stainless 2507 super-duplex (annealed) | Stainless | 29.008 | 0.3 | 7.222 | 79,770.8 | 0.3 | 17 | — | |
| Stainless 15-5 PH (H1025) | Stainless | 28.427 | 0.272 | 6 | 145,037.7 | 0.3 | 17.8 | — | |
| Stainless 13-8 Mo PH (H1000) | Stainless | 28.282 | 0.278 | 6 | 204,503.2 | 0.3 | 12.8 | — | |
| Stainless A286 (aged) | Stainless | 29.008 | 0.31 | 9.111 | 95,724.9 | 0.3 | 12.6 | — | |
| Nitronic 60 (annealed) | Stainless | 26.977 | 0.29 | 9.278 | 60,190.7 | 0.3 | 14.7 | — | |
| Stainless 904L (annealed) | Stainless | 27.557 | 0.3 | 8.5 | 31,908.3 | 0.3 | 11.5 | — | |
| Stainless 254 SMO (annealed) | Stainless | 28.282 | 0.3 | 9.167 | 43,511.3 | 0.3 | 13.5 | — | |
| Cast iron | |||||||||
| Gray cast iron G3000 brittle | Cast iron | 14.504 | 0.26 | 5.833 | 30,022.8 | 0.3 | 50 | — | |
| Ductile iron 65-45-12 | Cast iron | 24.511 | 0.275 | 6.444 | 44,961.7 | 0.3 | 33 | — | |
| Aluminum | |||||||||
| Aluminum 6061-T6 | Aluminum | 9.993 | 0.33 | 13.111 | 40,030.4 | 0.1 | 167 | — | |
| Aluminum 7075-T6 | Aluminum | 10.399 | 0.33 | 13 | 72,954 | 0.1 | 130 | — | |
| Aluminum 2024-T4 | Aluminum | 10.588 | 0.33 | 12.889 | 46,992.2 | 0.1 | 121 | — | |
| Aluminum A356-T6 (cast) | Aluminum | 10.501 | 0.33 | 11.944 | 26,977 | 0.1 | 151 | — | |
| Aluminum 6063-T5 | Aluminum | 9.993 | 0.33 | 13 | 21,030.5 | 0.1 | 209 | — | |
| Aluminum 5052-H32 | Aluminum | 10.196 | 0.33 | 13.222 | 27,992.3 | 0.1 | 138 | — | |
| Aluminum 2017-T4 | Aluminum | 10.501 | 0.33 | 13.111 | 40,030.4 | 0.1 | 134 | — | |
| Aluminum 7050-T7451 | Aluminum | 10.399 | 0.33 | 13.056 | 68,022.7 | 0.1 | 157 | — | |
| Aluminum 7475-T651 | Aluminum | 10.196 | 0.33 | 13 | 67,007.4 | 0.1 | 163 | — | |
| Aluminum 6082-T6 | Aluminum | 10.153 | 0.33 | 13.333 | 36,259.4 | 0.1 | 170 | — | |
| Aluminum 2219-T87 | Aluminum | 10.602 | 0.33 | 12.5 | 56,999.8 | 0.1 | 120 | — | |
| Aluminum 5083-H116 | Aluminum | 10.196 | 0.33 | 13.222 | 31,183.1 | 0.1 | 117 | — | |
| Aluminum 6005A-T6 | Aluminum | 10.008 | 0.33 | 12.778 | 32,633.5 | 0.1 | 188 | — | |
| Aluminum MIC-6 cast tooling plate | Aluminum | 10.298 | 0.33 | 13.611 | 17,984.7 | 0.1 | 142 | — | |
| Copper alloy | |||||||||
| Brass C360 | Copper alloy | 14.069 | 0.34 | 11.389 | 18,129.7 | 0.3 | 115 | — | |
| Bronze C932 (bearing) | Copper alloy | 14.504 | 0.34 | 10 | 18,129.7 | 0.3 | 59 | — | |
| Phosphor bronze C510 | Copper alloy | 15.954 | 0.34 | 9.889 | 55,114.3 | 0.3 | 84 | — | |
| Beryllium copper C17200 | Copper alloy | 18.565 | 0.3 | 9.889 | 159,541.5 | 0.3 | 105 | — | |
| Copper C101 | Copper alloy | 16.969 | 0.34 | 9.444 | 10,152.6 | 0.3 | 391 | — | |
| Aluminum bronze C95200 (952) | Copper alloy | 15.954 | 0.32 | 9 | 24,656.4 | 0.3 | 50 | — | |
| Cartridge brass C260 (H02) | Copper alloy | 15.954 | 0.35 | 11.056 | 50,038 | 0.3 | 120 | — | |
| Commercial bronze C220 (H02) | Copper alloy | 16.969 | 0.33 | 10.222 | 44,961.7 | 0.3 | 119 | — | |
| Naval brass C464 (O61 annealed) | Copper alloy | 14.504 | 0.34 | 11.778 | 24,656.4 | 0.3 | 116 | — | |
| Aluminum bronze C630 (C63000) | Copper alloy | 17.405 | 0.34 | 9 | 50,038 | 0.3 | 39 | — | |
| Nickel-aluminum bronze C955 (C95500, as-cast) | Copper alloy | 15.954 | 0.32 | 9 | 42,060.9 | 0.3 | 42 | — | |
| Cupronickel 90-10 C706 (C70600, annealed) | Copper alloy | 19.58 | 0.32 | 9.5 | 15,954.2 | 0.3 | 45 | — | |
| Cupronickel 70-30 C715 (C71500, annealed) | Copper alloy | 21.756 | 0.34 | 9 | 20,305.3 | 0.3 | 29 | — | |
| Manganese bronze C863 (C86300, cast) | Copper alloy | 14.069 | 0.33 | 12 | 60,190.7 | 0.3 | 35 | — | |
| Silicon bronze C655 (C65500, annealed) | Copper alloy | 14.939 | 0.34 | 10 | 21,030.5 | 0.3 | 36 | — | |
| Leaded bronze C937 (C93700, cast) | Copper alloy | 10.994 | 0.33 | 10 | 17,984.7 | 0.3 | 47 | — | |
| Chromium copper C182 (C18200, TH04) | Copper alloy | 16.969 | 0.33 | 9.778 | 65,267 | 0.3 | 324 | — | |
| Copper-nickel-tin C72900 (AT, spinodal) | Copper alloy | 21.03 | 0.33 | 9.111 | 89,923.4 | 0.3 | 38 | — | |
| Titanium | |||||||||
| Titanium Ti-6Al-4V | Titanium | 16.505 | 0.342 | 4.778 | 127,633.2 | 0.2 | 6.7 | — | |
| Titanium CP Grade 2 | Titanium | 15.229 | 0.37 | 4.778 | 39,885.4 | 0.2 | 17 | — | |
| Titanium Grade 1 CP (annealed) | Titanium | 14.939 | 0.34 | 4.778 | 24,656.4 | 0.2 | 16 | — | |
| Titanium Grade 4 CP (annealed) | Titanium | 15.084 | 0.34 | 5.389 | 69,618.1 | 0.2 | 17 | — | |
| Titanium Ti-6Al-4V ELI (Grade 23, annealed) | Titanium | 16.534 | 0.342 | 5.111 | 115,305 | 0.2 | 6.7 | — | |
| Titanium Ti-3Al-2.5V (Grade 9, annealed) | Titanium | 15.519 | 0.3 | 5.222 | 69,618.1 | 0.2 | 7.5 | — | |
| Titanium Ti-5Al-2.5Sn (Grade 6, annealed) | Titanium | 15.954 | 0.31 | 5.222 | 119,656.1 | 0.2 | 7.8 | — | |
| Titanium Ti-6Al-2Sn-4Zr-2Mo (6-2-4-2, duplex annealed) | Titanium | 16.534 | 0.32 | 4.278 | 124,732.5 | 0.2 | 7.1 | — | |
| Titanium Ti-15V-3Cr-3Al-3Sn (Beta, solution treated) | Titanium | 11.893 | 0.32 | 4.722 | 111,679.1 | 0.2 | 8.1 | — | |
| Nickel | |||||||||
| Inconel 718 (aged) | Nickel | 29.008 | 0.29 | 7.222 | 150,114.1 | 0.3 | 11 | — | |
| Monel 400 | Nickel | 26.107 | 0.32 | 7.722 | 34,809.1 | 0.3 | 22 | — | |
| Inconel 625 (annealed) | Nickel | 30.023 | 0.278 | 7.111 | 66,717.4 | 0.3 | 9.8 | — | |
| Inconel 600 (annealed) | Nickel | 30.023 | 0.29 | 7.389 | 42,060.9 | 0.3 | 14.9 | — | |
| Inconel X-750 (aged) | Nickel | 30.893 | 0.29 | 7 | 120,381.3 | 0.3 | 12 | — | |
| Hastelloy C-276 (annealed) | Nickel | 29.733 | 0.31 | 6.222 | 51,488.4 | 0.3 | 9.9 | — | |
| Waspaloy (aged) | Nickel | 30.603 | 0.3 | 6.778 | 115,305 | 0.3 | 11 | — | |
| Incoloy 800H (annealed) | Nickel | 28.427 | 0.34 | 8 | 29,732.7 | 0.3 | 11.5 | — | |
| Incoloy 825 (annealed) | Nickel | 28.427 | 0.29 | 7.722 | 39,160.2 | 0.3 | 11.1 | — | |
| Rene 41 (aged) | Nickel | 31.618 | 0.31 | 6.722 | 153,740 | 0.3 | 9 | — | |
| Nimonic 90 (aged) | Nickel | 30.893 | 0.31 | 7.056 | 101,526.4 | 0.3 | 11.5 | — | |
| MP35N (annealed) | Nickel | 33.794 | 0.3 | 7.111 | 60,045.6 | 0.3 | 11.2 | — | |
| Cobalt alloy | |||||||||
| Stellite 6 (cast) brittle | Cobalt alloy | 30.313 | 0.3 | 6.333 | 78,320.4 | 0.3 | 14.8 | — | |
| Haynes 188 (annealed) | Cobalt alloy | 33.649 | 0.3 | 6.889 | 67,297.5 | 0.3 | 10.4 | — | |
| L605 / Haynes 25 (annealed) | Cobalt alloy | 32.633 | 0.29 | 6.833 | 64,541.8 | 0.3 | 9.4 | — | |
| Refractory metal | |||||||||
| Molybdenum (wrought) | Refractory metal | 46.412 | 0.31 | 2.667 | 72,518.9 | 0.4 | 138 | — | |
| TZM molybdenum alloy (stress-relieved) | Refractory metal | 47.137 | 0.31 | 2.944 | 124,732.5 | 0.4 | 126 | — | |
| Tungsten (wrought) | Refractory metal | 59.611 | 0.28 | 2.5 | 108,778.3 | 0.7 | 173 | — | |
| Tantalum (annealed) | Refractory metal | 26.977 | 0.34 | 3.5 | 25,961.8 | 0.6 | 57 | — | |
| Niobium (annealed) | Refractory metal | 15.229 | 0.4 | 4.056 | 15,229 | 0.3 | 53.7 | — | |
| Light & specialty | |||||||||
| Magnesium AZ31B | Light & specialty | 6.527 | 0.35 | 14.444 | 31,908.3 | 0.1 | 96 | — | |
| Invar 36 (low-α) | Light & specialty | 20.45 | 0.29 | 0.667 | 40,030.4 | 0.3 | 10 | — | |
| Tungsten carbide (6% Co) brittle | Light & specialty | 87.023 | 0.22 | 2.778 | 435,113.2 | 0.5 | 86 | — | |
| Magnesium AZ91D (die cast) | Light & specialty | 6.527 | 0.35 | 14.444 | 21,755.7 | 0.1 | 72.7 | — | |
| Magnesium ZK60A-T5 | Light & specialty | 6.527 | 0.29 | 14.444 | 41,335.8 | 0.1 | 121 | — | |
| Magnesium WE43B-T6 | Light & specialty | 6.382 | 0.27 | 15 | 23,931.2 | 0.1 | 51 | — | |
| Beryllium S-200F (vacuum hot pressed) | Light & specialty | 43.946 | 0.08 | 6.278 | 34,809.1 | 0.1 | 200 | — | |
| Zirconium 702 (R60702, annealed) | Light & specialty | 14.359 | 0.35 | 3.278 | 30,022.8 | 0.2 | 22 | — | |
| Zinc die-cast Zamak 3 (ASTM AG40A) | Light & specialty | 13.924 | 0.25 | 15.222 | 30,167.9 | 0.2 | 113 | — | |
| Lead (chemical/pure, Pb) | Light & specialty | 2.321 | 0.44 | 16.056 | 797.7 | 0.4 | 35 | — | |
| Tin (pure, Sn) | Light & specialty | 7.252 | 0.36 | 12.222 | 1,740.5 | 0.3 | 67 | — | |
| Controlled expansion | |||||||||
| Kovar (Fe-Ni-Co) | Controlled expansion | 20.015 | 0.317 | 3.056 | 50,038 | 0.3 | 17.3 | — | |
| Alloy 42 (Fe-42Ni) | Controlled expansion | 21.466 | 0.29 | 2.944 | 36,259.4 | 0.3 | 10.7 | — | |
| Babbitt / white metal | |||||||||
| Babbitt tin-base (AMS 4800) | Babbitt / white metal | 7.687 | 0.33 | 12.778 | 4,351.1 | 0.3 | 34 | — | |
| Babbitt lead-base (B23 Gr.13) | Babbitt / white metal | 4.206 | 0.36 | 14.444 | 3,335.9 | 0.4 | 24 | — | |
| Self-lubricating | |||||||||
| Sintered bronze SAE 841 | Self-lubricating | 7.252 | 0.27 | 10.278 | 11,022.9 | 0.2 | 30 | — | |
| Sintered iron SAE 863 | Self-lubricating | 11.603 | 0.25 | 6.944 | 17,404.5 | 0.2 | 35 | — | |
| Graphalloy (graphite/metal) brittle | Self-lubricating | 1.885 | 0.2 | 2.5 | 14,503.8 | 0.1 | 20 | — | |
| Ceramic | |||||||||
| Alumina 96% brittle | Ceramic | 43.511 | 0.21 | 4.556 | 50,038 | 0.1 | 25 | — | |
| Alumina 99.5% brittle | Ceramic | 53.954 | 0.22 | 4.667 | 54,969.3 | 0.1 | 35 | — | |
| Silicon carbide (sintered SiC) brittle | Ceramic | 59.465 | 0.14 | 2.222 | 55,114.3 | 0.1 | 125 | — | |
| Silicon nitride (Si3N4) brittle | Ceramic | 44.962 | 0.27 | 1.833 | 101,526.4 | 0.1 | 30 | — | |
| Zirconia 3Y-TZP (yttria-stabilized) brittle | Ceramic | 30.458 | 0.3 | 5.833 | 145,037.7 | 0.2 | 2.5 | — | |
| Magnesia-PSZ zirconia (Mg-PSZ) brittle | Ceramic | 29.733 | 0.3 | 5.778 | 94,274.5 | 0.2 | 2.7 | — | |
| Boron carbide (B4C) brittle | Ceramic | 65.267 | 0.18 | 2.778 | 58,015.1 | 0.1 | 35 | — | |
| Aluminum nitride (AlN) brittle | Ceramic | 47.862 | 0.24 | 2.5 | 46,412.1 | 0.1 | 170 | — | |
| Silicon (single-crystal) brittle | Ceramic | 18.855 | 0.28 | 1.444 | 23,931.2 | 0.1 | 150 | — | |
| Sapphire (single-crystal Al2O3) brittle | Ceramic | 50.038 | 0.27 | 2.944 | 58,015.1 | 0.1 | 42 | — | |
| Macor (machinable glass-ceramic) brittle | Ceramic | 9.703 | 0.29 | 5.167 | 13,633.5 | 0.1 | 1.5 | — | |
| Cordierite brittle | Ceramic | 10.153 | 0.22 | 1.111 | 9,282.4 | 0.1 | 3 | — | |
| Glass | |||||||||
| Fused silica (quartz glass) brittle | Glass | 10.588 | 0.17 | 0.306 | 7,542 | 0.1 | 1.4 | — | |
| Borosilicate glass (Borofloat 33 / Pyrex) brittle | Glass | 9.282 | 0.2 | 1.806 | 3,625.9 | 0.1 | 1.2 | — | |
| Soda-lime glass brittle | Glass | 10.443 | 0.23 | 5 | 14,503.8 | 0.1 | 1 | — | |
| Composite | |||||||||
| Phenolic (linen Garolite LE) brittle | Composite | 1.044 | 0.2 | 10 | 12,473.2 | 0 | 0.3 | — | |
| G-10 / FR-4 (epoxy-glass) | Composite | 2.611 | 0.18 | 8.889 | 37,999.9 | 0.1 | 0.3 | — | |
| Carbon-fiber / epoxy (quasi-isotropic) | Composite | 7.252 | 0.31 | 1.667 | 36,114.4 | 0.1 | 5 | — | |
| Nylon 6/6, 33% glass-filled | Composite | 1.305 | 0.38 | 13.889 | 26,106.8 | 0 | 0.3 | — | |
| PEEK, 30% carbon-filled | Composite | 3.481 | 0.4 | 8.889 | 32,488.5 | 0.1 | 0.9 | — | |
| Polymer | |||||||||
| PEEK (unfilled) | Polymer | 0.522 | 0.38 | 26.111 | 14,503.8 | 0 | 0.3 | — | |
| Acetal / POM (Delrin) | Polymer | 0.45 | 0.35 | 61.111 | 9,427.5 | 0.1 | 0.3 | — | |
| Nylon 6/6 (dry) | Polymer | 0.421 | 0.39 | 44.444 | 11,603 | 0 | 0.3 | — | |
| PTFE (Teflon) | Polymer | 0.073 | 0.46 | 75 | 3,625.9 | 0.1 | 0.3 | — | |
| UHMW-PE | Polymer | 0.102 | 0.46 | 83.333 | 3,045.8 | 0 | 0.4 | — | |
| HDPE | Polymer | 0.145 | 0.42 | 83.333 | 3,771 | 0 | 0.5 | — | |
| Polycarbonate (PC) | Polymer | 0.334 | 0.37 | 37.778 | 8,992.3 | 0 | 0.2 | — | |
| PEI / Ultem 1000 | Polymer | 0.435 | 0.36 | 31.111 | 15,229 | 0 | 0.2 | — | |
| PPS (Ryton) | Polymer | 0.479 | 0.38 | 27.778 | 10,152.6 | 0 | 0.3 | — | |
| PVDF (Kynar) | Polymer | 0.247 | 0.4 | 72.222 | 7,251.9 | 0.1 | 0.2 | — | |
| Polyimide (Vespel SP-1) | Polymer | 0.45 | 0.41 | 30 | 12,473.2 | 0.1 | 0.4 | — | |
| Nylon 6 (cast, dry) | Polymer | 0.479 | 0.4 | 44.444 | 12,183.2 | 0 | 0.3 | — | |
| PET (Ertalyte) | Polymer | 0.45 | 0.4 | 33.333 | 12,328.2 | 0.1 | 0.3 | — | |
| Polypropylene (PP) | Polymer | 0.203 | 0.42 | 50 | 4,786.2 | 0 | 0.2 | — | |
| PMMA / acrylic brittle | Polymer | 0.464 | 0.37 | 38.889 | 10,152.6 | 0 | 0.2 | — | |
| Polysulfone (PSU / Udel) | Polymer | 0.363 | 0.37 | 31.111 | 10,152.6 | 0 | 0.3 | — | |
2 · Analysis — turn the knobs, watch it respond
Min safety factor: 3.24 · Max von Mises: 29,344.1 psi · axial strain εz = 0 µε (free ends, net axial force = 0)
Stress through the wall (radius spans every layer). Drag any knob → the gauges and graph update live.
Grab a knob — this sweeps it across its range; the dashed line marks where you are now.
Lift ΔØ along the sleeve: the band bulges, the lands sit on the press line until the oil peels them, the workpiece caps the lift at its clearance. Thick overlays mark live contact.
von Mises at the two wall faces along the sleeve — the band-edge bending spike and the weld clamping moment are the 3-D effects a uniform-section solve cannot see.
| Condition A — no workpiece: max oil pressure at SF ≥ 1.5 | 8,653.2 psi (charge ≈ 8,653.2 psi) |
| bare sleeve at the current charge | peak vM 42,292 psi at the band edge · SF 2.25 |
| Condition B — workpiece mounted: grip on Workpiece | contact 1.09 in · mean 1,745 psi · 47.3 ft·lbf |
| sleeve→body path (seated lands) | 0.28 in seated per land · mean 1,729 psi · 18.7 ft·lbf |
| joint rating (weaker friction path; welds in reserve) | 18.7 ft·lbf — land press fit governs |
| with the part on: peak vM | 27,919 psi · SF 3.4 |
| ends (both welded) & axial | Nx 81.63 kN/m tension · end close-in 0.00002 in Ø vs seat · boundary layer 1/β ≈ 0.17 in |
Drag to orbit · scroll to zoom. The cutaway shows the through-wall field; the skins carry the face stresses. Deformation exaggerated ×65. Peak vM 27,919 psi vs σy(sleeve) 95,000 psi — re-solved live at every knob turn.
Drag to orbit · scroll to zoom. Each arrow lies along the local σ1 (most-tensile principal) direction; length tracks |σ1| and color its signed level — tension vs compression. Hoop rings where ring stretch rules; near welds and band edges the bending + transverse-shear tilt rotates the arrows into the wall. Geometry undeformed. σ1 spans 10,484 … 27,322 psi — re-solved live at every knob turn.
I · In-plane field (Airy). Axisymmetric plane elasticity derives from the Airy stress function φ(r): σr = φ′/r, σθ = φ″, with ∇⁴φ = 0. The single-valued axisymmetric biharmonic is φ = A ln r + C r² (the r²ln r term is dropped — it carries a multivalued displacement), which is exactly Lamé’s field: σr = A/r² + 2C, σθ = −A/r² + 2C. Fixing A, C from the face pressures and integrating Hooke’s law gives every stiffness this panel uses: the sleeve’s own ring stiffness ks = Et/R̄² (thin limit) and the one-sided springs of the body and the workpiece (bore-loaded ring: k = E/{Ri[(Ro²+Ri²)/(Ro²−Ri²)+ν]}; OD-loaded: same bracket with −ν at Ro; solid shaft: k = E/[R(1−ν)]).
II · Axial structure. Let w(x) be the radial motion of the sleeve wall. Its energy per unit circumference is ∫[ ½D(w″)² + ½ksw² − q w ]dx with the plate rigidity D = Et³/12(1−ν²); stationarity gives the cylindrical-shell equation D wⅣ + ksw = q(x) — a beam on the Airy-derived elastic foundation. Disturbances heal over 1/β with β = [3(1−ν²)]¼/√(R̄t); under the band the particular solution is the membrane lift wm = pR̄²/Et.
III · Edge redundants by Castigliano. A semi-infinite shell end-loaded by (P, M₀) stores U = (β/ks)[P² + 2βPM₀ + 2β²M₀²], so ∂U/∂P and ∂U/∂M₀ hand over the end influence coefficients. Splitting the band step into a uniform half (no bending) plus an antisymmetric half (w = w″ = 0 at the step) proves the step transfers by pure shear: M(edge) = 0, w(edge) = wm/2 exactly, Q₀ = kswm/4β, with peak band moment (p/4β²)e−π/4sin(π/4) and the “ends close in” dip −0.0335 wm at βη = 3π/4 just outside the band. Pressure running to a welded end instead gives the classic clamp moment |M₀| = p/2β² and shear p/β.
IV · One-sided contacts. The lands obey qb = kb(δb−w) ≥ 0 (press fit that can peel, never pull) and the part qp = kp(w−c) ≥ 0 over its length — a linear complementarity problem on the shell operator, solved by an active-set iteration (loads and springs are weighted by Rface/R̄ so face line-loads map correctly to the midsurface). The welds tie the sleeve to the seated line and, because hoop tension Poisson-shortens the tube, pick up an axial force Nx = νEt mean(w)/[(1−ν²)R̄] from the closure ∫εxdx = 0.
IV-b · End conditions — the three BVPs. The variation δΠ leaves the
boundary terms [D w″·δw′] and [−D w‴·δw], so each end must take either the essential pair
(w = wseat, w′ = 0 — a weld) or the natural pair (M = −D w″ = 0, Q = −D w‴ = 0 — an unwelded end).
Both welded: essential at ±L/2; the weld pair reacts the Poisson shortening, Nx = νEt mean(w)/[(1−ν²)R̄];
pressure reaching a weld shows the p/2β² clamp moment. One welded: essential at one end, natural at the other; the clamp signature
appears on the welded side only, the free side carries the pure membrane (w = wm exactly under uniform pressure), and Nx = 0 —
a single weld has no partner to react the couple. No welds: natural at both ends — a uniformly pressurized free-free tube has
no boundary layer at all, and the press-fit lands alone retain the sleeve (axially by friction, unmodeled — verify separately).
Each case is gated in engine/test_sleeve.js Case 9: the free-free membrane to 10−11, the one-weld clamp to 2%.
V · 3-D stress recovery. σx(x,z) = Nx/t + 12M(x)z/t³; σθ(x,z) = Ew/R̄ + νσx;
σr interpolates the face tractions through the wall; von Mises of the triple governs. Every closed form above gates the numerical solver in
engine/test_sleeve.js (step transition to 0.2%, clamp moment to 2%, seated land = Lamé series springs to 0.1%, Clapeyron energy balance to 1%,
thick-wall engine cross-checks to ≤8%). References: Timoshenko & Woinowsky-Krieger ch. 15; Hetényi, Beams on Elastic Foundation;
Den Hartog, Advanced Strength of Materials; Roark ch. 13; Timoshenko & Goodier for Part I. The full write-up ships with the project as
docs/hydraulic-sleeve-derivation.md.
| Interface | Ø (in) | Interf. Ø (in) | Pressure (psi) | Assembly force (lbf) | Torque (ft·lbf) |
|---|---|---|---|---|---|
| 1 sealed oil | 1.102 | 0 | 5,801.5 | 0 | 0 |
| 2 | 1.26 | -0.0008 | 1,879.4 | 1,405.7 | 73.8 |
| Layer | Hoop @ID (psi) | Hoop @OD (psi) | Max von Mises (psi) | Safety factor | Status |
|---|---|---|---|---|---|
| 1 | -5,801.5 | -5,801.5 | 2,447.5 | 31.41 | elastic |
| 2 | 27,666.7 | 23,744.6 | 29,344.1 | 3.24 | elastic |
| 3 | 3,373.7 | 1,494.2 | 4,560.4 | 7.95 | elastic |
| Interface | Heat outer ΔT | or Cool inner ΔT |
|---|---|---|
| 1 | +104 °F (→172) | −112 °F (→-44) |
| 2 | +0 °F (→68) | −0 °F (→68) |
| Interface | Heat hub: window | Cool shaft: window |
|---|---|---|
| 1 | — | — |
| 2 | — | — |
| Operating T (°F) | Min contact p (psi) | Min SF | Status |
|---|---|---|---|
| -22 | 0 | — | clearance |
| 32 | 0 | — | clearance |
| 86 | 0 | — | clearance |
| 140 | 0 | — | clearance |
| 194 | 0 | — | clearance |
| 248 | 0 | — | clearance |
| 302 | 0 | — | clearance |
| 356 | 0 | — | clearance |
| 410 | 0 | — | clearance |
| 464 | 0 | — | clearance |
| 518 | 0 | — | clearance |
Notes
Engine: N-layer compound-cylinder solver (Lamé thick-wall, multi-interface coupled solve via Eigen, compiled to
WebAssembly). Contact is unilateral — an interface flagged clearance has
separated under the given loads/temperatures. Safety factor = material yield ÷ peak von Mises (set σy
via the material). Suggested-fit limits use the ISO 286 tables from the source workbook; validated to <0.1%.
Elastic-plastic analysis (opt-in, in Loads & options) runs an incremental flow-theory solve
(von Mises J2 or Tresca; perfectly-plastic or with linear strain hardening set per material via a tangent modulus
Et) for the true post-yield state: it caps
stress at the yield surface, grows a plastic zone from the bore, relieves the contact pressure, and reports the
residual stress and the gross-yield (limit-load) margin — the factor by which the whole load can scale before a
member becomes fully plastic, found numerically. The standard first-yield safety factor remains a valid
conservative basis; the limit-load margin governs once a member is allowed to yield locally. A fit that exceeds
gross-yield collapse is flagged.
The hardening model chooses how a hardened material re-yields when the operating loads are
removed: isotropic grows the yield surface (reverse yield delayed by the full
How It Works
A hydraulic arbor is an interference fit you can switch on and off. A thin sleeve is welded to the body around an annular oil chamber; a setscrew piston (or a factory charge) pressurizes the trapped oil and the sleeve bulges elastically as a free ring — a few hundredths of a millimetre is plenty. That motion closes the small fitting clearance to the part, and every bit of pressure past lift-off becomes contact pressure at the grip; friction riding on that pressure holds the torque, exactly the thick-wall (Lamé) mechanics of a press fit. This page runs the same N-layer engine as the Press-Fit Designer with the oil film as one more unilateral interface — OD grip puts the chamber under the sleeve so it expands into a workpiece bore (expanding arbor / mandrel); ID grip puts the chamber outside the sleeve so it contracts onto a tool shank (expansion chuck). Because the ends are welded, the oil is a closed spring: temperature and outside squeeze re-solve its operating pressure through the trapped volume.
Key Components
- Body — the arbor or chuck core; carries the galleries and the charge screw. Stiff by design so the sleeve does the moving.
- Expansion sleeve — the thin wall that does the work; welded or brazed at both ends to seal the chamber. Wall thickness is the key trade: thin lifts far but yields early (run the Wall study).
- Oil chamber & galleries — the annular gap plus drillings and the screw bore; their total volume is the “Oil volume” input and sets the oil-spring stiffness of the sealed system.
- Charge screw / piston with seals — sets the charge pressure; on toolholders it is the wrench flat on the side of the chuck.
- The gripped surface — workpiece bore over the sleeve (OD grip) or tool shank inside it (ID grip). Its tolerance must land inside the sleeve’s lift window — h6/g6-class fits in practice.
Common Configurations
- Expanding arbor / mandrel (OD grip) — locates gears, rings and bearing races on their bores for turning, grinding and inspection; runout in single microns.
- Hydraulic expansion toolholder (ID grip) — grips drill, reamer and endmill shanks; the oil film also damps vibration, improving surface finish and tool life (SCHUNK’s TENDO line is the classic example).
- Double-sleeve locking bushings — one charge grips ID and OD at once for hub-to-shaft connections; that case has its own sheet: Hydraulic Bushing Design.
- Workholding fixtures — multiple small arbors plumbed to one supply for clamping thin-wall parts without distortion.
Advantages and Limitations
- Advantages: micron-level concentricity and repeatability; part change in seconds with no press or oven; uniform all-around pressure that does not lobe thin rings; the oil film damps chatter; grip is adjustable and fully reversible.
- Limitations: the part tolerance must sit inside the lift window (≈0.01–0.03 mm on Ø for typical sleeves) — a sloppy bore never seals the grip; a sealed charge loses pressure as it warms less than it gains squeeze, but hot spindles do walk the grip (check the Fit-vs-temperature tab); the thin sleeve sets a hard pressure ceiling at yield (use Max @ SF); and static rigidity is below a shrunk joint of the same size — heavy interrupted cuts favor shrink-fit holders.
References & further reading
- SCHUNK — TENDO hydraulic expansion toolholders — the standard ID-grip implementation and its application data.
- ETP Transmission — hydraulic hub–shaft connections and expanding mandrels (OD grip).
- Wikipedia — Interference fit — the underlying friction-joint mechanics.
- Wikipedia — Cylinder stress (Lamé equations) — the elasticity this engine solves.
- Wikipedia — Fluid bearing — background on pressurized films between surfaces.
Disclaimer
Recommendations on application design and material selection are based on available technical data and are offered as suggestions only. Each user should make their own tests to determine the suitability for their own particular use. Standards Applied LLC offers no express or implied warranties concerning the form, fit, or function of a product in any application.
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